US3444878A - Fluid control device - Google Patents

Description

y 0, 1969 E. A. MAYER 3,444,878

FLUID CONTROL DEVI CE Filed April 4. 1966 Sheet of 5 SUPPLY P SUR 25 RCE j gP i 20 38 F i2 0 4|; P2 D2 i\\\\\\\\\\\\\\\\ 3 P i (T s s s LOAD INVENTOR. ENDRE A. MAYER Sheet SUPPLYPRESSURE 4/25 SOURCE May 20, 1969 E. A. MAYER FLUID CONTROL DEVICE Filed April 4, 1966 CONTROL PRESSURE '50 souRcE LOAD 76 y 20, 1969 E. A. MAYER 3,444,878

FLUID CONTROL DEVICE Filed April 4, 1966 ISheet 3 of 5 P =75 PSI I50 \4 g P3 PSI PC'PS INVENTOR.

ENDRE A. MAYER y 0, 1969 E. A. MAYER 3,444,878

FLUID CONTROL DEVICE Filed April 4, 1966Sheet 4 of 5 a? PRESSURE ag 0 SOURCE SOUR l g7 (80 1 76-40 Q 82 f I A1 a 2o GAUGE 'Tls 1 ENTO- E EA.M R

Fl'G-4 May 20, 1969 E. A. MAYER 3,444,878

FLUID CONTROL DEVICE Filed April 4, 1966Sheet 5 of 5 SOJM MECHANICAL INPUT RATE DEG/SEC PRESSURE GAUGE H8 OUTPUT PSI MECHANICAL INPUT RATE DEG/SEC OUTPUT PSI PRESSURE GAUGE INVENTOR. ENDRE A. MAYER United States Patent 3,444,878 FLUID CONTROL DEVICE Endre A. Mayer, Birmingham, Mich., assignor to The Bendix Corporation, a corporation of Delaware Filed Apr. 4, 1966, Ser. No. 539,761

Int. Cl. Fc 1/08 US. Cl. 137-815 11 Claims ABSTRACT OF THE DISCLOSURE The pressure amplifier having a vortex chamber with a centrally located outlet hole in combination with a probe axially displaced downstream of the outlet hole connected to a source of counterflow fluid.

This invention pertains to a fluid control device and more particularly to a fluid vortex device wherein a supply pressure is subjected to a control pressure which causes the supply pressure to experience a vortical motion resulting in an output that is reduced in proportion to the vortical motion.

Fluid vortex devices are generally known in the art. They comprise a cylindrical chamber, an inlet for introducing supply fluid to the chamber, an axially disposed outlet for discharge of fluid from the chamber and a control port for introducing control fluid tangentially into the chamber to impart rotational velocity or vorticity to the fluid flowing through the chamber. Introduction of the control fluid, which occurs when control pressure is greater than supply pressure, imparts a rotational velocity to the fluid in the chamber which produces a reduction in the amount of fluid emerging from the outlet and a reduction in output pressure. The amount of fluid emerging and output pressure decrease as the rotational velocity is increased.

In the preferred embodiment described below, there is an output pickup tube which is axially displaced from the center of the vortex and receives an output flow from the vortex. The pressure in the output tube is lower than the pressure in the center of the vortex, and the chamber surrounding the outlet tube is vented through a valve to atmosphere or other pressure less than supply pressure. The following objects will refer to this type of vortex device.

It is an object of this invention to provide in a vortex device as described above, an area of extremely high gain in a low control input area thereby making the device very suitable as a rotational rate sensor.

It is an object to provide in such a fluid control device reduced noise so that the device has higher sensitivity.

It is an object of this invention to accomplish the high gain and reduced noise by introducing a fluid flow in the output tube which is counter to the output flow in the tube.

It is an object of this invention to connect, by means of a fluid connection, the center of the vortex to the output tube, thereby establishing substantially the same pressure in the output tube as in the center of the vortex thereby providing the above-mentioned counterflow from an internal pressure source.

It is an object of this invention to provide the abovementioned counterflow by connecting an external pressure source to the output tube.

It is an object of this invention to provide valves in the output chamber vent, the counterflow line connecting the center of the vortex and the output pickup tube, and the output line which is connected to the counterflow line to obtain maximum performance from the fluid device.

These and other objects will become more apparent when a preferred embodiment is described in connection with the drawings in which:

FIGURE 1 is a partially sectioned schematic view of a preferred embodiment of this invention taken at 11 of FIGURE 2;

FIGURE 1a is a modification of FIGURE 1 wherein the pressure to provide the counterflow in the output tube is derived from a separate external pressure source;

FIGURE 2 is a section taken at 2-2 of FIGURE 1;

FIGURE 3 is a chart showing the vortex center pressure P the output tube pressure P and the output pressure P vs. the control pressure P minus the supply pressure P which is provided to supply the vortical flow;

FIGURE 4 is a sectioned view of a partial schematic of a second embodiment of this invention which is adapted as a rotational rate sensor;

FIGURE 4a is a section partially filled in elevational view of the rotational coupler;

FIGURE 5 is an output curve of a device similar to that shown in FIGURE 4; and

FIGURE 5a is an output curve of a prior art device.

Embodiment of FIGURE 1 In FIGURE 1 is shown a fluid vortex device having an outer tubular member housing aninner cylinder 22 and having aninput passage 24 which is connected to asupply pressure source 25 for supp-lying a pressure P Passage 24 is connected toannular groove 26 which carries the supply flow and is in communication withchamber 30 throughannulus 28.

Chamber 30 is defined by the end ofcylinder 22 anddisc 32 withdisc 32 being supported intubular housing 20 by a secondtubular member 34.Disc 32 has an opening 36 centrally thereof.

Acylinder 38 is positioned centrally oftubular member 34 and has anannular flange 40 which is in connection with acentral opening 41 inmember 38 to provide an output pickup tube. Achamber 42 is provided aroundtube 40 and avent 44vents chamber 42 to atmosphere.

Also formed intubular member 20 iscontrol port 46 which is connected through a valve 48 to acontrol pressure source 50 which supplies control pressure P There may beadditional ports 46 supplied with control pressure P Supply pressure P causes a flow which passes throughtube 24,annuli 26, 28,chamber 30, opening 36, to outputtube 40. The flow fromannulus 26 to opening 36 is radial when there is no control flow fromport 46. A control flow is developed when the control pressure P inport 46 exceeds the supply pressure P inport 24 causing a swirl or vortical flow of air inannulus 28 andchamber 30, which develops a back pressure reducing the pressure at the center of the vortex which would be in the center ofchamber 30.

The output flow from opening 36 tooutput tube 40 is a straight flow when there is no control flow fromport 46, and fans out or becomes conical as a control flow occurs fromport 46. The amount of fanning, or angle of the cone, increases as the vortical flow, due to increasing control pressure fromport 46, increases. The higher the vortical flow, the less flow will be directed to outputpickup tube 40 and therefore the lower the pressure inpickup tube 40.

The portion of the device of FIGURES 1 and 2 thus described is improved upon by this invention by structure which applies a counterflow inpassage 41 andtube 40 which is a fluid flow from left to right in the view of FIG-URE 1. In other words, by raising the pressure intube 40 to approximately that which it is in the center ofchamber 30, a pressure is obtained which is slightly higher than the pressure of the fluid from opening 36, resulting in the counterflow.

In the preferred embodiment of FIGURE 1, the pressure totube 40 is raised to that at the center ofchamber 30 by providing a 'bleed 50 in the center ofcylinder 22 which is also the center of chamber 30'. Flow from bleed 50 passes throughpassage 52 incylinder 22, fluid line 54,valve 56, andpassage 41. In this manner, the pressure at the center ofchamber 30 is presented at tube 40'.Output line 60 is connected to line 58 and passes fluid to a valve 62 which is connected to load 64 byline 66. Output pressure P is present inline 66. Avalve 68 is attached tovent 44 which affects the pressure P inchamber 42.

Satisfactory results have been obtained with thevalve 68 opening between .7D and SD where D is the diameter of opening 36, with 1.5D being typical. Also,valve 56 may have an opening between zero and D with a typical opening being .3D Valve 56 is very important in obtaining the desired characteristics of this invention and along withvalve 68, is adjusted to obtain the desired gain noise level and linear range desired for a particular application. For example, the gain may be increased by openingvalve 56. Valve 62 is an impedance matching device which alters the output impedance of the device to match load impedance.

Also, satisfactory results have been obtained with the following dimensional relationships where D is the diam eter of opening 36, D is the inside diameter oftube 40, D is the inside diameter ofpassage 50, S is the distance between the end oftube 40 and the left side ofdisc 32 while L is the distance between the end ofcylinder 22 and the right side ofdisc 32.

SED]. DzED D "=".8 Of D1 LE33D1.

With the device of FIGURE 1, the curves of FIGURE 3 were obtained. With the supply pressure P equal to 75 pounds per square inch gauge, the three curves P P and P were obtained. P is the pressure inpassage 52, P is the pressure inpassage 41 and P is the pressure inline 66. The abscissa of the graph is in pounds per square inch and is the control pressure P minus the supply pressure P The ordinate of the graph is pressure in pounds per square inch gauge (p.s.i.g.).

As can be seen, the curves P P and P are gradually lower as the control pressure increasingly exceeds the supply pressure. However, it can be seen that output pressure P has a very high gain ratio in the area of .5 p.s.i. on the abscissa. This means that for a slight increase in control pressure P a very large decrease in output pressure P results. Hence, the device is especially suitable for rotational rate sensors where the rotation rate of a member such astubular element 20 in FIGURE 1 is desired to be detected. (An embodiment specifically designed for rate sensing is shown in FIGURES 4 and 4a and will be later described.) Of course, other applications requiring high gain at low control pressures can be made with the device of this invention.

Changing the supply pressure will result in curves similar to P P and P but with lower supply pressures resulting in curves below those shown in FIGURE 3 and higher supply pressures resulting in curves higher than those shown in FIGURE 3. Also, the vent pressure P may be changed by regulatingvalve 68.

Embodiment of FIGURE Ia The counterflow intube 40 may also be applied from a separate external pressure as shown in FIGURE 1a where anexternal pressure source 70 is connected to a valve 72 which in turn is connected to apassage 41 to supply the added pressure to result in the counterflow. In this embodiment, the load 76 is connected to line 78 and the same results of high gain in low control pressure input are obtained.

Embodiment 0 FIGURE 4 FIGURE 4 shows an embodiment wherein the swirl or the vortical flow is obtained by rotation of the device, with the output varying according to the rotation rate.

An outer cup shaped housing has aport 82 formed therein which is connected to apressure source 84. Acentral bleed 86 is formed in the cover face ofcup 80. Aport 87 admits flow from bias pressure source 87a to establish a zero rate flow approximately at the 11ndpoint M of the high gain portion HG of curve P in FIGURE 3. Rotational rate in one direction will cause an output between M and H and rotational rate in the other diretcion will cause an output between M and G.

Cylindrical insert 88 is positioned incup 80 and spaced therefrom to form annulus 90 andchamber 92. Also,annular space 94 communicates withpassage 82 and is formed betweencup 80 andinsert 88.Annular space 96, also formed betweencup 80 andinsert 88, provides communication betweenannulus 94, and the supply pressure P and annulus 90.

Positioned ininsert 88 is cylinder havingannular flange 102 which defines the output pickoif tube.Tube 102 is connected to line 104 which communicates withbleed 86 so that the pressure at the center of chamber 92-is presented intube 102 causing a counterflow, or flow from left to right, therein. An insert 105 is positioned centrally ofcylinder 88 and has opening 106 connected to a flaredpassage 107.Vent passages 108 are connected throughvalve 109 to atmosphere.

Annular coupling element 110 is located in annulus 90 and is porous, as shown in FIGURE 4a, so that whenhousing 80 is rotated, the air in annulus 90 will also be rotated increasing the efliciency of this device when used as a rotational rate sensor.

In the operation of the device shown in FIGURE 4, rotation is applied tohousing 80 causing a swirl of air in annulus 90 altering the output of air flow intube 102 and bleed 86 with this output being read ongauge 118. The greater the rotational rate, the smaller will be the output reading atpressure gauge 118.

The graph of FIGURE 5 shows mechanical input motion and pressure gauge output reading atgauge 118. The input mechanical motion is shown in the upper portion of the graph of FIGURE 5 with the ordinate being in degrees per second and the abscissa being in time. With the device being rotated at 50 per second, a first pressure output A ofgauge 118 is obtained; at 0 rotation per second, a pressure ouput A of gauge 11 8 is obtained; and

at a rotation of minus 50 per second, a third pressure A atgauge 118 is obtained. Also, when the rotation rate is continuously changed, as shown by the sine wave curve in the input portion of the graph of FIGURE 5, a corresponding sine wave in p.s.i. ofgauge 118 results.

The same mechanical input was applied to a device that did not have the counter flow intube 102 and the results are recorded in the graph of FIGURE 5a. It is seen that the output p.s.i. has much more noise therein and is much less distinct making it less sensitive and therefore less useful.

It is not definitely known why the device of this invention provides the superior gain shown in FIGURE 3 and the significantly reduced noise shown in FIGURE 5 but it is felt that the counterflow of air intube 40 of the device of FIGURE 1, andtube 102 of the device of FIG-URE 4, tends to stabilize the cone of air that is formed on the output of theopening 36 in FIGURE 1 or in theflare passage 107 of FIGURE 4 thereby minimizing instability, pressure changes, and noise to increase and improve the fluid properties of devices incorporating the teaching of this invention.

Although this invention has been disclosed and illustrated with reference to particular applications, the principles involved are susceptible of numerous other applications which will be apparent to persons skilled in the art. The invention is, therefore, to be limited only as indicated by the scope of the appended claims.

Having thus described my invention, I claim:

1. Apparatus comprising v a housing having a cylindrical chamber therein,

a fluid input passage being connected to said chamber to provide a fluid flow into said chamber,

fluid control passage for causing the flow from said input passage to experience a vortical flow in said chamber,

a fluid output chamber passage being exposed to the center of said cylindrical chamber to receive the discharge of said chamber and provide downstream thereof a diverging rotating flow,

a fluid output tube axially aligned with and spaced from the fluid output passage in the path of the discharge flow from said output passage,

counterflow means to supply said output tube with a flow counter to the flow in said output passage,

load passage means being connected to said counterflow means with the pressure in said load passage means being responsive to the counterflow means pressure and the characteristics of the load means pressure being improved thereby.

2. The apparatus ofclaim 1 with said counterflow means comprising an external pressure source being connected to said output tube to supply said counterflow from said fluid output passage.

3. The apparatus ofclaim 1 with valve means being connected to said load passage means for adjusting the flow to said load means thereby providing an impedance matching device in said load means passage.

4. The apparatus ofclaim 1 with a second chamber for providing an enclosed volume between said fluid output tube and said fluid output passage,

vent passage means being positioned in said second chamber,

valve means being connected to said vent passage means to provide a controllable pressure in said second chamber.

5. The apparatus ofclaim 4 with said valve means having an opening in the range between .7D and 3D where D is the output passage diameter.

6. The apparatus ofclaim 1 with valve means being connected to said counterflow means upstream from said load means for adjusting the flow in said counter flow means.

7. The apparatus of claim 6 with said valve means having an opening in the range between zero and D where D is the output passage diameter.

8. The apparatus ofclaim 1 with said counterflow means comprising a central opening to said cylindrical chamber opposite said fluid output passage and said central opening being connected to said fluid output tube to provide said output tube with a pressure that is greater than the pressure from said fluid output passage.

9. The apparatus of claim 8 with the output passage having a diameter of D the spacing S between the output passage and the output tube being approximately equal to D the inside diameter D of the output tube being approximately equal to D the axial length L between the output passage and the central opening being approximately 3.3D

the inside diameter D of the central opening being approximately equal to .8D

10. The apparatus of claim 8 with the output passage having a diameter of D the spacing S between the output passage and the output tube being approximately equal to D 11. The apparatus of claim 8 with the output passage having a diameter of D the inside diameter D of the output tube being approximately equal to D References Cited UNITED STATES PATENTS 3,181,546 5/1965 Boothe 13781.5 3,207,168 9/1965 Warren 137-815 3,219,048 11/1965 Palmisano 137-81.5 3,256,899 6/1966 Dexter et al. 137-81.5 3,267,946 8/1966 Adams et al. 137-81.5 3,272,215 9/1966 'Bjornsen et a1 l3781.5 3,290,947 12/ 1966 Reilly 137--81.5 XR 3,324,891 6/ 1967 Rhoades 137-81.5 XR 3,336,931 8/1967 Fox et al. 137-81.5

SAMUEL SCOTT, Primary Examiner.

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